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CAMACHO, Emanuel A. R. et al. Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, v. 36, n. 1, p. 1-11, 2024Tradução . . Disponível em: https://dx.doi.org/10.1063/5.0185716. Acesso em: 03 out. 2024.
APA
Camacho, E. A. R., Silva, M. M. da, Silva, A. R. R., & Marques, F. D. (2024). Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, 36( 1), 1-11. doi:10.1063/5.0185716
NLM
Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 out. 03 ] Available from: https://dx.doi.org/10.1063/5.0185716
Vancouver
Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 out. 03 ] Available from: https://dx.doi.org/10.1063/5.0185716
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SILVA, Gabriel Pereira Gouveia da. Experimental assessment of aerodynamic and aeroacoustic interaction effects of wingtip-mounted propellers. 2023. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2023. Disponível em: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-08112023-174940/. Acesso em: 03 out. 2024.
APA
Silva, G. P. G. da. (2023). Experimental assessment of aerodynamic and aeroacoustic interaction effects of wingtip-mounted propellers (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de https://www.teses.usp.br/teses/disponiveis/18/18161/tde-08112023-174940/
NLM
Silva GPG da. Experimental assessment of aerodynamic and aeroacoustic interaction effects of wingtip-mounted propellers [Internet]. 2023 ;[citado 2024 out. 03 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-08112023-174940/
Vancouver
Silva GPG da. Experimental assessment of aerodynamic and aeroacoustic interaction effects of wingtip-mounted propellers [Internet]. 2023 ;[citado 2024 out. 03 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-08112023-174940/
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SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Finite wing effects on the energy harvesting from stall-induced oscillations. Journal of Vibration and Control, p. 1-17, 2022Tradução . . Disponível em: https://doi.org/10.1177/10775463221089732. Acesso em: 03 out. 2024.
APA
Santos, C. R. dos, & Marques, F. D. (2022). Finite wing effects on the energy harvesting from stall-induced oscillations. Journal of Vibration and Control, 1-17. doi:10.1177/10775463221089732
NLM
Santos CR dos, Marques FD. Finite wing effects on the energy harvesting from stall-induced oscillations [Internet]. Journal of Vibration and Control. 2022 ; 1-17.[citado 2024 out. 03 ] Available from: https://doi.org/10.1177/10775463221089732
Vancouver
Santos CR dos, Marques FD. Finite wing effects on the energy harvesting from stall-induced oscillations [Internet]. Journal of Vibration and Control. 2022 ; 1-17.[citado 2024 out. 03 ] Available from: https://doi.org/10.1177/10775463221089732
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 03 out. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2019-3850
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2019-3850
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ZAKARIA, Mohamed Y et al. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments. IOP Conference. Series: Materials Science and Engineering. Bristol, United Kingdom: IOP Publishing. Disponível em: https://doi.org/10.1088/1757-899X/610/1/012098. Acesso em: 03 out. 2024. , 2019
APA
Zakaria, M. Y., Santos, C. R. dos, Dayhoum, A., Marques, F. D., & Hajj, M. R. (2019). Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments. IOP Conference. Series: Materials Science and Engineering. Bristol, United Kingdom: IOP Publishing. doi:10.1088/1757-899X/610/1/012098
NLM
Zakaria MY, Santos CR dos, Dayhoum A, Marques FD, Hajj MR. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments [Internet]. IOP Conference. Series: Materials Science and Engineering. 2019 ; 610 1-15.[citado 2024 out. 03 ] Available from: https://doi.org/10.1088/1757-899X/610/1/012098
Vancouver
Zakaria MY, Santos CR dos, Dayhoum A, Marques FD, Hajj MR. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments [Internet]. IOP Conference. Series: Materials Science and Engineering. 2019 ; 610 1-15.[citado 2024 out. 03 ] Available from: https://doi.org/10.1088/1757-899X/610/1/012098
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CHAIM, Victor Cheidde. System identification and robust controller design for category 3 rotary-wing UAV. 2018. Dissertação (Mestrado) – Universidade de São Paulo, São Carlos, 2018. . Acesso em: 03 out. 2024.
APA
Chaim, V. C. (2018). System identification and robust controller design for category 3 rotary-wing UAV (Dissertação (Mestrado). Universidade de São Paulo, São Carlos.
NLM
Chaim VC. System identification and robust controller design for category 3 rotary-wing UAV. 2018 ;[citado 2024 out. 03 ]
Vancouver
Chaim VC. System identification and robust controller design for category 3 rotary-wing UAV. 2018 ;[citado 2024 out. 03 ]
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SILVA, Gabriel Pereira Gouveia da e EGUEA, João Paulo e CATALANO, Fernando Martini. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811. Acesso em: 03 out. 2024.
APA
Silva, G. P. G. da, Eguea, J. P., & Catalano, F. M. (2018). Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
NLM
Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 out. 03 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
Vancouver
Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 out. 03 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
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CHREIM, José Rodolfo et al. Changes in modern lifting-line methods for swept wings and viscous effects. 2018, Anais.. Red Hook, NY: Curran Associates, 2018. Disponível em: https://doi.org/10.2514/6.2018-3170. Acesso em: 03 out. 2024.
APA
Chreim, J. R., Pimenta, M. de M., Dantas, J. L. D., & Assi, G. R. da S. (2018). Changes in modern lifting-line methods for swept wings and viscous effects. In Papers. Red Hook, NY: Curran Associates. doi:10.2514/6.2018-3170
NLM
Chreim JR, Pimenta M de M, Dantas JLD, Assi GR da S. Changes in modern lifting-line methods for swept wings and viscous effects [Internet]. Papers. 2018 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2018-3170
Vancouver
Chreim JR, Pimenta M de M, Dantas JLD, Assi GR da S. Changes in modern lifting-line methods for swept wings and viscous effects [Internet]. Papers. 2018 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2018-3170
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PEREIRA, Lourenço Tércio Lima et al. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3458. Acesso em: 03 out. 2024.
APA
Pereira, L. T. L., Botero Bolívar, L., Araujo, M. T. de, Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3458
NLM
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2018-3458
Vancouver
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/6.2018-3458
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BOCCATO, Bruno Ribeiro e BRAVO-MOSQUERA, Pedro David e CATALANO, Fernando Martini. Análise dos efeitos aerodinâmicos do Canard em uma aeronave militar não convencional. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1349/813. Acesso em: 03 out. 2024.
APA
Boccato, B. R., Bravo-Mosquera, P. D., & Catalano, F. M. (2018). Análise dos efeitos aerodinâmicos do Canard em uma aeronave militar não convencional. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1349/813
NLM
Boccato BR, Bravo-Mosquera PD, Catalano FM. Análise dos efeitos aerodinâmicos do Canard em uma aeronave militar não convencional [Internet]. Anais. 2018 ;[citado 2024 out. 03 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1349/813
Vancouver
Boccato BR, Bravo-Mosquera PD, Catalano FM. Análise dos efeitos aerodinâmicos do Canard em uma aeronave militar não convencional [Internet]. Anais. 2018 ;[citado 2024 out. 03 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1349/813
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SOUZA, Joabe Marcos de e CATALANO, Fernando Martini. Multi-disciplinary design optimization of a blended winglet. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf. Acesso em: 03 out. 2024.
APA
Souza, J. M. de, & Catalano, F. M. (2018). Multi-disciplinary design optimization of a blended winglet. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
NLM
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
Vancouver
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
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BRAVO MOSQUERA, Pedro David e ABDALLA, Alvaro Martins e CATALANO, Fernando Martini. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf. Acesso em: 03 out. 2024.
APA
Bravo Mosquera, P. D., Abdalla, A. M., & Catalano, F. M. (2018). Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
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CAIXETA JUNIOR, Paulo Roberto e MARQUES, Flavio Donizeti. Multiobjective optimization of an aircraft wing design with respect to structural and aeroelastic characteristics using neural network metamodel. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 40, p. 1-11, 2018Tradução . . Disponível em: https://doi.org/10.1007/s40430-017-0958-7. Acesso em: 03 out. 2024.
APA
Caixeta Junior, P. R., & Marques, F. D. (2018). Multiobjective optimization of an aircraft wing design with respect to structural and aeroelastic characteristics using neural network metamodel. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 40, 1-11. doi:10.1007/s40430-017-0958-7
NLM
Caixeta Junior PR, Marques FD. Multiobjective optimization of an aircraft wing design with respect to structural and aeroelastic characteristics using neural network metamodel [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2018 ; 40 1-11.[citado 2024 out. 03 ] Available from: https://doi.org/10.1007/s40430-017-0958-7
Vancouver
Caixeta Junior PR, Marques FD. Multiobjective optimization of an aircraft wing design with respect to structural and aeroelastic characteristics using neural network metamodel [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2018 ; 40 1-11.[citado 2024 out. 03 ] Available from: https://doi.org/10.1007/s40430-017-0958-7
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ANAYA, Maribel et al. Damage classification based on machine learning applications for an unmanned aerial vehicle. 2017, Anais.. Stanford, CA, USA: Stanford University, 2017. Disponível em: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf. Acesso em: 03 out. 2024.
APA
Anaya, M., Cerón Muñoz, H. D., Vitola, J., Tibaduiza, D. A., & Pozo, F. (2017). Damage classification based on machine learning applications for an unmanned aerial vehicle. In Proceedings. Stanford, CA, USA: Stanford University. Recuperado de https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
NLM
Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
Vancouver
Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
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CATALANO, Fernando Martini et al. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016, Anais.. Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics, 2016. . Acesso em: 03 out. 2024.
APA
Catalano, F. M., Abdalla, A. M., Cerón Muñoz, H. D., & Munjulury, R. C. (2016). Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. In . Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics.
NLM
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 out. 03 ]
Vancouver
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 out. 03 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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CERÓN MUÑOZ, Hernán Darío et al. Experimental analyses of droop, wingtips and fences on a BWB model. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 03 out. 2024.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Bravo Mosquera, P. D., & Catalano, F. M. (2016). Experimental analyses of droop, wingtips and fences on a BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2024 out. 03 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2024 out. 03 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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CERÓN MUÑOZ, Hernán Darío et al. Aerodynamic interference of wingtip and wing devices on BWB model. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 03 out. 2024.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Solarte Pineda, J., & Catalano, F. M. (2014). Aerodynamic interference of wingtip and wing devices on BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2024 out. 03 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2024 out. 03 ]
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MORALEDA, F. P. e CATALANO, Fernando Martini. Experimental analysis of the aerodynamics of porous flap side-edge. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 03 out. 2024.
APA
Moraleda, F. P., & Catalano, F. M. (2014). Experimental analysis of the aerodynamics of porous flap side-edge. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2024 out. 03 ]
Vancouver
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2024 out. 03 ]
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CERÓN MUÑOZ, Hernán Darío et al. Experimental investigation of wing-tip devices on the reduction of induced drag. Journal of Aircraft, v. 50, n. 2, p. 441-449, 2013Tradução . . Disponível em: https://doi.org/10.2514/1.C031862. Acesso em: 03 out. 2024.
APA
Cerón Muñoz, H. D., Cosin, R., Coimbra, R. F. de F., Correa, L. G. N., & Catalano, F. M. (2013). Experimental investigation of wing-tip devices on the reduction of induced drag. Journal of Aircraft, 50( 2), 441-449. doi:10.2514/1.C031862
NLM
Cerón Muñoz HD, Cosin R, Coimbra RF de F, Correa LGN, Catalano FM. Experimental investigation of wing-tip devices on the reduction of induced drag [Internet]. Journal of Aircraft. 2013 ; 50( 2): 441-449.[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/1.C031862
Vancouver
Cerón Muñoz HD, Cosin R, Coimbra RF de F, Correa LGN, Catalano FM. Experimental investigation of wing-tip devices on the reduction of induced drag [Internet]. Journal of Aircraft. 2013 ; 50( 2): 441-449.[citado 2024 out. 03 ] Available from: https://doi.org/10.2514/1.C031862
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MOREIRA, Emilio Eduardo Tressoldi et al. Attitude estimation using MEMS IMU and magnetometer data with PI filter. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. . Acesso em: 03 out. 2024.
APA
Moreira, E. E. T., Schwening, G. S., Souza, M. M. de, De Salvi, F. T. B., Carlos, S. R., Belo, E. M., et al. (2013). Attitude estimation using MEMS IMU and magnetometer data with PI filter. In Anais. Rio de Janeiro, RJ: ABCM.
NLM
Moreira EET, Schwening GS, Souza MM de, De Salvi FTB, Carlos SR, Belo EM, Breganon R, Lemes RC. Attitude estimation using MEMS IMU and magnetometer data with PI filter. Anais. 2013 ;[citado 2024 out. 03 ]
Vancouver
Moreira EET, Schwening GS, Souza MM de, De Salvi FTB, Carlos SR, Belo EM, Breganon R, Lemes RC. Attitude estimation using MEMS IMU and magnetometer data with PI filter. Anais. 2013 ;[citado 2024 out. 03 ]